GB9823018D0 - Die cutting composite laminate - Google Patents
Die cutting composite laminateInfo
- Publication number
- GB9823018D0 GB9823018D0 GBGB9823018.8A GB9823018A GB9823018D0 GB 9823018 D0 GB9823018 D0 GB 9823018D0 GB 9823018 A GB9823018 A GB 9823018A GB 9823018 D0 GB9823018 D0 GB 9823018D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- laminate
- die
- die cutting
- composite laminate
- cutting composite
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
Links
- 239000002131 composite material Substances 0.000 title 1
- 239000012530 fluid Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B26—HAND CUTTING TOOLS; CUTTING; SEVERING
- B26D—CUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
- B26D5/00—Arrangements for operating and controlling machines or devices for cutting, cutting-out, stamping-out, punching, perforating, or severing by means other than cutting
- B26D5/08—Means for actuating the cutting member to effect the cut
- B26D5/12—Fluid-pressure means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B26—HAND CUTTING TOOLS; CUTTING; SEVERING
- B26F—PERFORATING; PUNCHING; CUTTING-OUT; STAMPING-OUT; SEVERING BY MEANS OTHER THAN CUTTING
- B26F1/00—Perforating; Punching; Cutting-out; Stamping-out; Apparatus therefor
- B26F1/38—Cutting-out; Stamping-out
- B26F1/40—Cutting-out; Stamping-out using a press, e.g. of the ram type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/545—Perforating, cutting or machining during or after moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Life Sciences & Earth Sciences (AREA)
- Forests & Forestry (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
Abstract
The method comprises positioning a die (16) on the laminate (10) with the laminate in an uncured or part-cured condition, applying a covering (24) to the die (16) and laminate (10) and applying fluid, such as gas, under pressure to the covering (24) to load the die sufficiently to cut through the laminate. In one preferred embodiment the die (16) is left in position after cutting the laminate (10) to form a liner for the cut formed by the die (16).
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB9823018.8A GB9823018D0 (en) | 1998-10-22 | 1998-10-22 | Die cutting composite laminate |
JP2000578142A JP2002528278A (en) | 1998-10-22 | 1999-10-20 | Composite laminate cutting |
PCT/GB1999/003461 WO2000024553A1 (en) | 1998-10-22 | 1999-10-20 | Composite laminate cutting |
AU63519/99A AU6351999A (en) | 1998-10-22 | 1999-10-20 | Composite laminate cutting |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB9823018.8A GB9823018D0 (en) | 1998-10-22 | 1998-10-22 | Die cutting composite laminate |
Publications (1)
Publication Number | Publication Date |
---|---|
GB9823018D0 true GB9823018D0 (en) | 1998-12-16 |
Family
ID=10841000
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB9823018.8A Ceased GB9823018D0 (en) | 1998-10-22 | 1998-10-22 | Die cutting composite laminate |
Country Status (4)
Country | Link |
---|---|
JP (1) | JP2002528278A (en) |
AU (1) | AU6351999A (en) |
GB (1) | GB9823018D0 (en) |
WO (1) | WO2000024553A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108583842A (en) * | 2018-03-09 | 2018-09-28 | 彩虹无人机科技有限公司 | A kind of composite material light lid mechanism for film covering |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0117804D0 (en) | 2001-07-21 | 2001-09-12 | Bae Systems Plc | Aircraft structural components |
DE102004032554B4 (en) * | 2004-07-06 | 2006-07-13 | Airbus Deutschland Gmbh | Closure for closing a component opening in a component |
JP5478289B2 (en) * | 2010-02-10 | 2014-04-23 | 三菱航空機株式会社 | Opening closure member, aircraft |
JP5378260B2 (en) * | 2010-02-10 | 2013-12-25 | 三菱航空機株式会社 | Opening closure member, aircraft |
ES2400768B1 (en) * | 2010-06-30 | 2014-02-12 | Airbus Operations, S.L. | INTERNAL AIRCRAFT STRUCTURE IN COMPOSITE MATERIAL. |
GB2485758B (en) * | 2010-09-22 | 2013-03-13 | Gkn Aerospace Services Ltd | Net edge method |
CN105000164B (en) * | 2015-07-10 | 2017-09-19 | 常州市科宏电子电器有限公司 | A kind of preparation method of water-impervious aircraft safety inspection cover and lid |
GB2604126A (en) * | 2021-02-24 | 2022-08-31 | Airbus Operations Ltd | Reinforced holes |
CN114770982B (en) * | 2022-03-28 | 2023-04-11 | 航天特种材料及工艺技术研究所 | Combined positioning mechanism and positioning method thereof |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4291816A (en) * | 1980-07-09 | 1981-09-29 | Canadair Limited | Fuel tank access door for aircraft |
JPH0665480B2 (en) * | 1988-03-08 | 1994-08-24 | キヤノン電子株式会社 | Punching method and punching die for plate member in which resin material is mixed with reinforcing material such as fiber fiber |
WO1991017035A1 (en) * | 1990-04-30 | 1991-11-14 | Ontario Die Company Of America | Method and apparatus for producing structural injection moldings |
JP2829776B2 (en) * | 1990-07-19 | 1998-12-02 | 日本無機株式会社 | Manufacturing method of inorganic fiber soundproofing material |
TW266186B (en) * | 1992-05-01 | 1995-12-21 | Martin Marietta Corp |
-
1998
- 1998-10-22 GB GBGB9823018.8A patent/GB9823018D0/en not_active Ceased
-
1999
- 1999-10-20 JP JP2000578142A patent/JP2002528278A/en active Pending
- 1999-10-20 WO PCT/GB1999/003461 patent/WO2000024553A1/en active Application Filing
- 1999-10-20 AU AU63519/99A patent/AU6351999A/en not_active Abandoned
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108583842A (en) * | 2018-03-09 | 2018-09-28 | 彩虹无人机科技有限公司 | A kind of composite material light lid mechanism for film covering |
CN108583842B (en) * | 2018-03-09 | 2020-07-14 | 彩虹无人机科技有限公司 | Composite material light cover mechanism for film skin |
Also Published As
Publication number | Publication date |
---|---|
AU6351999A (en) | 2000-05-15 |
WO2000024553A1 (en) | 2000-05-04 |
JP2002528278A (en) | 2002-09-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AT | Applications terminated before publication under section 16(1) |